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  • Hypersonic vehicle simulation model [microform] : winged-cone configuration / John D. Shaughnessy ... [et al.].

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
    • 1990

  • Advanced ascent guidance study [microform] : ascent guidance for a winged boost vehicle / by Michael A. Corvin.

    • Text
    • Cambridge, Mass. : Charles Stark Draper Laboratory ; [Washington, D.C.? : National Aeronautics and Space Administration ; Springfield, Va.? : National Technical Information Service, distributor, 1988]
    • 1988

  • Optimal guidance law develpment for an advanced launch system [microform] / Anthony J. Calise and Martin S.K. Leung.

    • Text
    • Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
    • 1995

  • Ascent trajectory dispersion analysis for WTR heads-up space shuttle trajectory [microform] : final technical report.

    • Text
    • Huntsville, Ala. : Dynetics, Inc. ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Ascent/descent ancillary data production user's guide [microform] / prepared by H.R. Brans, A.W. Seacord, J.W. Ulmer.

    • Text
    • Houston, Tex. : System Development Division, TRW Defense Systems Group ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1986]
    • 1986

  • Near-optimal operation of dual-fuel launch vehicles [microform] / M. Ardema and H.-C. Chou, J. Bowles.

    • Text
    • Reston, VA : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
    • 1996

  • Wind models for the NSTS ascent trajectory biasing for wind load alleviation [microform] / by O.E. Smith ... [et al.].

    • Text
    • [Marshall Space Flight Center, Ala.] : National Aeronautics and Space Administration, George C. Marshall Space Flight Center ; [Springfield, Va. : For sale by National Technical Information Service, 1989]
    • 1989
    • 1 Resource

    Available Online

    http://purl.access.gpo.gov/GPO/LPS92623

  • Integrating the Base of Aircraft Data (BADA) in CTAS trajectory synthesizer / Michael Abramson, Kareem Ali.

    • Text
    • Moffett Field, California : National Aeronautics and Space Administration, Ames Research Center, September 2012.
    • 2012-9
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo52896

  • Mars sample return : Mars Ascent Vehicle mission & technology requirements / Jeffrey V. Bowles [and three others].

    • Text
    • Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, November 2013.
    • 2013-11
    • 1 Resource

    Available Online

    https://purl.fdlp.gov/GPO/gpo54688

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